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Performance tests and simulations for Taiji-1 inertial sensor
International Journal of Modern Physics A ( IF 1.4 ) Pub Date : 2021-04-09 , DOI: 10.1142/s0217751x2140011x
Jian Min 1 , Jun-Gang Lei 1 , Yun-Peng Li 1 , Dong-Xue Xi 1 , Wen-Ze Tao 1 , Cun-Hui Li 1 , Xiao-Qing Zhang 1 , Zuo-Lei Wang 1 , Da Fan 2 , Zi-Ren Luo 3 , Jun-Biao Wang 3 , Zhi Wang 4 , Ke-Qi Qi 4 ,
Affiliation  

Taiji-1 satellite was successfully launched on 31 August 2019, and it has been operating normally in orbit until now. A series of in-orbit experiments were carried out with the inertial sensor, which included the micro-thrust test, drag-free control test and laser interferometer test. Comprehensive performance simulations and tests of the inertial sensor were also carried out prior to the launch of Taiji-1, including the calibration and drop-tower tests. These tests were one of the preconditions for the success of these experiments. The calibration experiments were conducted in a cave-lab using the gravity-inclination method and the scale factors of the inertial sensor along Y- and Z-axis were measured. In addition, 20 drop-tower tests were carried out in the National Microgravity Laboratory of China (NMLC) drop tower and the control stability of all the axes was tested and optimized. A simulation model was used before each test, and the results showed that an accurate simulation prior to each experiment had an important role in ensuring the efficiency and accuracy of the experiment. The circuit-gain switch was realized for the first time during the drop-tower tests. The test results indicated that the microgravity level of the NMLC drop tower could reach about 13 μg0 along the horizontal axes, offering an important reference for researchers planning to conduct microgravity experiments in the NMLC drop tower.
更新日期:2021-04-09
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